Abstract
The object of research is the effect of sintering under pressure (10 MPa–4.1 GPa) on the formation of the structure and properties of ZrB 2 , HfB 2 , and composites on their bases. It has been found that high pressure consolidation results in an improvement of mechanical characteristics. In particular, the hardness and fracture toughness of the materials sintered under 4.1 GPa pressure are higher than those of the materials obtained under hot pressing conditions at 20–30 MPa and spark-plasma sintering at 50 MPa. High-pressure sintered HfB 2 demonstrated hardness H V (9.8 N)=21.3±0.8 GPa, H V (49 N)=19.3±1.3 GPa, and H V (98 N)=19.2±0.5 GPa and fracture toughness K 1C (49 N)=7.2 MPa · m 0.5 and K 1C (98 N)=5.7 MPa · m 0.5 . The HfB 2 sintered by hot pressing at 1850 °C and 30 MPa demonstrated hardness: H V (9.8 N)= 19.0 GPa , H V (49 N)= 18.7 GPa, and H V (98 N)=18.1 GPa, K 1C (9.8 N)=7.7 MPa · m 0.5 , K 1C (49 N)=6.6 MPa · m 0.5 and K 1C (98 N)=5.3 MPa · m 0.5 . High pressure sintered ZrB 2 (a=0.3167 nm, c=0.3528 nm, γ=6.2 g/cm 3 ) demonstrated H V (9.8 N)=17.7±0.6 GPa, H V (49 N)=15.4±1.2 GPa, and H V (98 N)=15.3±0.36 GPa and K 1C (9.8 N)=4.3 MPa · m 0.5 , K 1C (49 N)=4.2 MPa · m 0.5 and K 1C (98 N)=4.0 MPa · m 0.5 . Addition of 20 wt. % of SiC to ZrB 2 and sintering under high pressure (4.1 GPa) allowed essential increase of hardness to H V (9.8 N)=24.2±0.7 GPa, H V (49 N)=16.7±0.5 GPa, and H V (98 N)=17.6±0.4 GPa and fracture toughness to K 1C (49 N)=7.1 MPa · m 0.5 , K 1C (98 N)=6.2 MPa·m 0.5 ; the material density was γ=5.03 g/cm 3 . Additions of SiC and Si 3 N 4 to ZrB 2 lead to some increase in fracture toughness (up to K 1C (98 N)=9.2 MPa · m 0.5 ). The developed ZrB 2 - and HfB 2 -based materials and composites can be used for aerospace applications, in cutting and refractory industries, etc.
Highlights
For the manufacture of supersonic aircraft mainly aluminum aviation alloys are used, and metal super alloys are used in more critical areas
The materials prepared under 4.1 GPa pressure demonstrated higher mechanical characteristics than that sintered under 20–30 MPa by hot pressing even at higher temperatures
The paper deals with investigation of pressure effect on the mechanical characteristics of the consolidated ZrB2, HfB2 and composit es on their bases with silicon carbide (SiC) and Si3N4 additions
Summary
For the manufacture of supersonic aircraft mainly aluminum aviation alloys are used, and metal super alloys are used in more critical areas (for example, for the manufacture of engine components). This material has high melting temperature >3000 °C [8], significant values of fracture strength, durability and heat resistance It has high thermal conductivity, which provides rapid heat removal and dissipation from the surface that is in contact with oxidative gas stream which is an extremely important advantage of composites based on ZrB2. The present paper deals with the mechanical characteristics (hardness and fracture toughness) study of high pressure (4 GPa) – high temperature (HP-HT) sintered ZrB2 and HfB2 ceramics and composites on their bases which are compared with that of ceramics and/or composites prepared by HotP and SPS methods. The aim of research is to study the correlations between manufacturing pressure (10 MPa–4.1 GPa) – temperature conditions, structure and mechanical characteristics of the consolidated ZrB2- and HfB2-based refractory materials
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